Approach and landing trajectory optimization for Reusable Launch Vehicle using Adaptive Gauss pseudo-spectral method
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- 英文论文题名：Approach and landing trajectory optimization for Reusable Launch Vehicle using Adaptive Gauss pseudo-spectral method
- 论文作者：Chaofan Zhang ; Qun Zong ; Qi Dong ; Bailing Tian ; Zhiyu Li ; Jing Zong
- 英文论文作者：Chaofan Zhang ; Qun Zong ; Qi Dong ; Bailing Tian ; Zhiyu Li ; Jing Zong ; School of Electrical and Information Engineering ; Tianjin University ; College of Precision Instrument and Opto-Electronics Engineering ; Tianjin University
- 年：2017
- 作者机构：School of Electrical and Information Engineering,Tianjin University;College of Precision Instrument and Opto-Electronics Engineering,Tianjin University;
- 英文论文关键词：Approach and Landing(A&L) ; reusable launch vehicle(RLV) ; adaptive Gauss pseudo-spectral(AGPM) ; trajectory optimization
- 会议召开时间：2017-07-26
- 会议录名称：第36届中国控制会议论文集（B）
- 英文会议录名称：Proceedings of the 36th Chinese Control Conference（B）
- 语种：英文
- 分类号：V448.2
- 学会代码：KZLL
- 会议名称：第36届中国控制会议
- 会议地点：中国辽宁大连
- 主办单位：中国自动化学会控制理论专业委员会
- 学会名称：中国自动化学会控制理论专业委员会
- 页数：6
- 文件大小：546k
- 原文格式：D
- 会议级别：全国
摘要
The Approach and Landing(A&L) trajectory optimization is important for reusable launch vehicle(RLV) to deliver it to its landing site safely and reliably. And the trajectory should satisfy multi-constraints and path features. In this paper, the 3D dynamics of RLV in the A&L phase is introduced.and the the adaptive Gauss pseudo-spectral method(AGPM) is used to solve the A&L trajectory optimization problem. The adaptive method in GPM can improve the accuracy of the trajectory and accelerate convergence velocity of algorithm effectively. The simulation results of the typical RLV(X-33) demonstrate the feasibility of the trajectory optimization scheme which can let the RLV land securely.
The Approach and Landing(A&L) trajectory optimization is important for reusable launch vehicle(RLV) to deliver it to its landing site safely and reliably. And the trajectory should satisfy multi-constraints and path features. In this paper, the 3D dynamics of RLV in the A&L phase is introduced.and the the adaptive Gauss pseudo-spectral method(AGPM) is used to solve the A&L trajectory optimization problem. The adaptive method in GPM can improve the accuracy of the trajectory and accelerate convergence velocity of algorithm effectively. The simulation results of the typical RLV(X-33) demonstrate the feasibility of the trajectory optimization scheme which can let the RLV land securely.
The Approach and Landing(A&L) trajectory optimization is important for reusable launch vehicle(RLV) to deliver it to its landing site safely and reliably. And the trajectory should satisfy multi-constraints and path features. In this paper, the 3D dynamics of RLV in the A&L phase is introduced.and the the adaptive Gauss pseudo-spectral method(AGPM) is used to solve the A&L trajectory optimization problem. The adaptive method in GPM can improve the accuracy of the trajectory and accelerate convergence velocity of algorithm effectively. The simulation results of the typical RLV(X-33) demonstrate the feasibility of the trajectory optimization scheme which can let the RLV land securely.
引文
[1]Zhao J,Zhou R.Reentry trajectory optimization for hypersonic vehicle satisfying complex constraints,Chinese Journal of Aeronautics,2013,26(6):1544-1553.
[2]Tian B,Fan W,Su R,et al.Real-Time Trajectory and Attitude Coordination Control for Reusable Launch Vehicle in Reentry Phase,Industrial Electronics IEEE Transactions on,2015,62(3):1639-1650.
[3]Yong E M,Tang G J,Chen L.Rapid trajectory optimization for hypersonic reentry vehicle via Gauss pseudospectral method,Yuhang Xuebao/journal of Astronautics,2008,29(6):1766-1772.
[4]Filipe N R S.Terminal area energy management trajectory optimization using interval analysis,In:AIAA Guidance,Navigation,and Control Conference.2008.
[5]Ridder S D,Mooij E.Terminal area trajectory planning using the energy-tube concept for reusable launch vehicles,Acta Astronautica,2011,68(7 8):915-930.
[6]Lan X J,Liu L,Wang Y J.Online trajectory planning and guidance for reusable launch vehicles in the terminal area,Acta Astronautica,2015,118:237–245.
[7]Horneman K,Kluever C.Terminal Area Energy Management Trajectory Planning for an Unpowered Reusable Launch Vehicle,in AIAA Atmospheric Flight Mechanics Conference and Exhibit.2013.
[8]Kluever C A.Unpowered Approach and Landing Guidance Using Trajectory Planning,Journal of Guidance Control&Dynamics,2004,27(6):967-974.
[9]AIAA.In-Flight TAEM/Final Approach Trajectory Generation for Reusable Launch Vehicles,in Infotech@Aerospace.2005.
[10]Barton G,Tragesser S.Autolanding trajectory design for the X-34,in 24th Atmospheric Flight Mechanics Conference.1999:4161
[11]Jiang Z,Ordónez R.Trajectory generation on approach and landing for RLVs using motion primitives and neighboring optimal control,in American Control Conference,2007.ACC'07.IEEE,2007:1091-1096.
[12]Jiang Z,Ordó?ez R.On-line robust trajectory generation on approach and landing for reusable launch vehicles,Automatica,2009,45(7):1668-1678.
[13]Su Z,Wang H.A novel robust hybrid gravitational search algorithm for reusable launch vehicle approach and landing trajectory optimization,Neurocomputing,2015,162:116-127.
[14]Reddien G W.Collocation at Gauss points as a discretization in optimal control,SIAM Journal on Control and Optimization,1979,17(2):298-306.
[15]Bollino K P.High-Fidelity Real-Time Trajectory Optimization for Reusable Launch Vehicles,Monterey California Naval Postgraduate School,2006.
[16]Sun Y,Hou M Z,Duan G R,et al.On-line optimal autonomous reentry guidance based on improved Gauss pseudospectral method,Science China Information Sciences,2014,57(5):1-16
[17]Yan H,He Y.Adaptive Integrated Guidance and Control Based on Backstepping for the Landing of Reusable Launch Vehicles,IFAC-Papers On Line,2015,48(28):496-501.
[18]Harl N,Balakrishnan S N.Reentry terminal guidance through sliding mode control,Journal of guidance,control,and dynamics,2010,33(1):186-199.
[2]Tian B,Fan W,Su R,et al.Real-Time Trajectory and Attitude Coordination Control for Reusable Launch Vehicle in Reentry Phase,Industrial Electronics IEEE Transactions on,2015,62(3):1639-1650.
[3]Yong E M,Tang G J,Chen L.Rapid trajectory optimization for hypersonic reentry vehicle via Gauss pseudospectral method,Yuhang Xuebao/journal of Astronautics,2008,29(6):1766-1772.
[4]Filipe N R S.Terminal area energy management trajectory optimization using interval analysis,In:AIAA Guidance,Navigation,and Control Conference.2008.
[5]Ridder S D,Mooij E.Terminal area trajectory planning using the energy-tube concept for reusable launch vehicles,Acta Astronautica,2011,68(7 8):915-930.
[6]Lan X J,Liu L,Wang Y J.Online trajectory planning and guidance for reusable launch vehicles in the terminal area,Acta Astronautica,2015,118:237–245.
[7]Horneman K,Kluever C.Terminal Area Energy Management Trajectory Planning for an Unpowered Reusable Launch Vehicle,in AIAA Atmospheric Flight Mechanics Conference and Exhibit.2013.
[8]Kluever C A.Unpowered Approach and Landing Guidance Using Trajectory Planning,Journal of Guidance Control&Dynamics,2004,27(6):967-974.
[9]AIAA.In-Flight TAEM/Final Approach Trajectory Generation for Reusable Launch Vehicles,in Infotech@Aerospace.2005.
[10]Barton G,Tragesser S.Autolanding trajectory design for the X-34,in 24th Atmospheric Flight Mechanics Conference.1999:4161
[11]Jiang Z,Ordónez R.Trajectory generation on approach and landing for RLVs using motion primitives and neighboring optimal control,in American Control Conference,2007.ACC'07.IEEE,2007:1091-1096.
[12]Jiang Z,Ordó?ez R.On-line robust trajectory generation on approach and landing for reusable launch vehicles,Automatica,2009,45(7):1668-1678.
[13]Su Z,Wang H.A novel robust hybrid gravitational search algorithm for reusable launch vehicle approach and landing trajectory optimization,Neurocomputing,2015,162:116-127.
[14]Reddien G W.Collocation at Gauss points as a discretization in optimal control,SIAM Journal on Control and Optimization,1979,17(2):298-306.
[15]Bollino K P.High-Fidelity Real-Time Trajectory Optimization for Reusable Launch Vehicles,Monterey California Naval Postgraduate School,2006.
[16]Sun Y,Hou M Z,Duan G R,et al.On-line optimal autonomous reentry guidance based on improved Gauss pseudospectral method,Science China Information Sciences,2014,57(5):1-16
[17]Yan H,He Y.Adaptive Integrated Guidance and Control Based on Backstepping for the Landing of Reusable Launch Vehicles,IFAC-Papers On Line,2015,48(28):496-501.
[18]Harl N,Balakrishnan S N.Reentry terminal guidance through sliding mode control,Journal of guidance,control,and dynamics,2010,33(1):186-199.